基于效能的舰艇电子对抗训练效果评估方法

摘 要：为解决舰艇电子对抗专业训练缺乏统一评估标准与方法体系等实际评估难题;采用系统分析方法结合舰艇电子对抗专业训练实际;研究提出了基于“任务要求分解”的作战效能量化指标体系构建方法、训练效果表达方法及实用评估指标体系、定量指标评估模型、评估标准等舰艇电子对抗训练效果评估方法体系;能够满足专业训练效果评估所需,对其它专业军事训练效果评估工作亦具有借鉴意义。     

内编队地球重力场测量性能数值分析

内编队系统通过实现内卫星纯引力轨道环境和内卫星精密定轨,完成高精度地球重力场测量,实现了不依赖于加速度计的重力卫星实施新途径。针对内编队重力场测量性能难以解析分析的情况,基于MATLAB并行程序设计进行了重力场测量数值模拟,获得了内编队重力场测量的有效阶数及其精度。在内编队轨道高度为300km、内卫星干扰力为1.0×10-10m/s2、外卫星定轨精度为3cm、内外卫星相对状态测量精度为1mm的条件下,计算得到内编队测量重力场的有效阶数为72,相应的大地水准面累积误差为44cm,重力异常累积误差为4.5mGal,由此可知内编队测量重力场的有效阶数主要分布在低阶部分。     

基于组合赋权雷达图实现电网电能质量综合评估

将改进的组合赋权雷达图方法用于电网电能质量综合评估。对主观、客观赋权法组合,基于组合权重与原权重之间的偏差尽可能小的优化思想,求取雷达图中各项指标的组合权值。利用各指标对应的扇形区域的对角线作为指标轴绘制雷达图,不仅最大限度体现各指标的独立权重,也反映了各指标之间的相互影响。利用雷达图的面积和周长两个变量完成对电能质量的综合评估。最后通过应用实例,验证了论文方法的合理性和在电能质量综合评估中的有效性。     

基于联合相似测度的SAR图像边缘点特征配准方法

针对SAR图像配准过程中几何变换影响特征匹配稳健性和适应性的问题,提出了一种在特征匹配过程中直接解算几何变换模型的边缘点特征配准方法。利用SAR图像边缘点的梯度和方向特征,基于像素迁移思想,定义了图像匹配的联合相似度——联合特征均方和(SSJF),并建立了SAR图像边缘点集相似性匹配准则;基于方向模板提出了改进的ROEWA算子;利用改进的遗传算法(GA)来进行相似度的全局优化搜索,获取配准模型参数;利用多幅SAR图像的配准试验,对本文方法的性能进行了验证。     

基于灰色AHP方法的综合航电系统效能

针对在对综合航电系统效能进行评估的过程中经常遇到多指标度量效能的情况,提出了一种将层次分析法和灰色系统理论相结合的效能评估方法,对航空电子系统中多指标度量效能进行评估.最后,通过实例计算表明使用这种方法获得的评估结果更加客观、科学,对综合航空电子系统效能的评估具有一定的参考价值.     

高焓高压空气加热器壁面传热过程数值计算

以一种高焓高压空气加热器为研究对象,对其冷却通道的流动和传热进行了三维数值仿真,冷却剂采用液态水,燃烧室和喷管分别采用不同的壁面材料,考虑壁面材料物性随温度的变化,并通过加热器热试验证了数值仿真结果的正确性。在此基础上,对比分析了气体辐射、冷却通道结构以及冷却水的流动方式对壁面换热的影响。结果表明:气体辐射对加热器燃烧室段壁面换热影响较大,对喷管壁面换热无明显的影响。在传热计算中,忽略气体辐射会引起较大的误差;冷却通道数和宽度存在最优组合,使得壁面换热量最大。冷却水的流动方式对燃气侧壁面温度影响较小,但对冷却液侧壁面温度的影响较大。     

要地防空指挥控制系统作战效能灰色聚类评估

建立要地防空指挥控制系统作战效能评估指标体系,运用层次分析法确定各层次指标权重,提出了一种基于灰色定聚类和中心点三角白化权函数的要地防空指挥控制系统作战效能灰色聚类评估方法,并通过算例对该方法的有效性进行了检验。结果表明该方法是切实可行的。     

结合平流层飞艇姿态的太阳辐射强度分布

平流层飞艇上表面太阳辐射强度的分布是影响光伏阵列输出性能的重要因素。为分析平流层飞艇飞行姿态对其上表面太阳辐射强度分布特征的影响,并建立飞艇动力学模型与太阳辐射物理模型交互耦合的计算模型。使用该模型对算例飞艇进行计算分析,量化得出飞艇偏航角和俯仰角耦合变化对飞艇表面太阳辐射强度分布影响的结果,并比较分析了太阳辐射强度受飞艇飞行姿态影响的特性。研究结果可用于指导太阳能电池阵在平流层飞艇上的优化布局和阵列构型。     

Thermal hazard assessment of TKX-50-based melt-cast explosive

In the present study, thermal hazards of TNT and DNAN used as the molten binder in TKX-50-based melt-cast explosives were comparatively studied through accelerating rate calorimeter (ARC) and Cook-off experiments. Two kinds of ARC operation modes were performed to investigate the thermal safety performance under adiabatic conditions (HWS mode) and constant heating (CHR mode). The obtained results demonstrated that at both heating modes, DNAN/TKX-50 outperformed TNT/TKX-50 from the thermal safety point of view. However, the sensitivity to heat of the samples was reverse because of the different heating modes. In addition, the results of thermal hazard assessment obtained from the cook-off experiment complied with ARC analysis which indicated the molten binder TNT replaced by DNAN would reduce the hazard of the TKX-50 melt cast explosive. Furthermore, the results of cook-off experiments also showed that DNAN/TKX-50 outperformed TNT/TKX-50 from the aspect of thermal stability, which was consistent with the result of CHR mode because of the similar heating process.     

Formation of adiabatic shearing band for high-strength Ti-5553 alloy: A dramatic thermoplastic microstructural evolution

By using split Hopkinson pressure bar, optical microscopy and electronic microscopy, we investigate the influence of initial microstructures on the adiabatic shear behavior of high-strength Ti–5Al–5V–5Mo–3Cr (Ti-5553) alloy with lamellar microstructure and bimodal microstructure. Lamellar alloy tends to form adiabatic shearing band (ASB) at low compression strain, while bimodal alloy is considerably ASB-resistant. Comparing with the initial microstructure of Ti-5553 alloy, we find that the microstructure of the ASB changes dramatically. Adiabatic shear of lamellar Ti-5553 alloy not only results in the formation of recrystallized β nano-grains within the ASB, but also leads to the chemical redistribution of the alloying elements such as Al, V, Cr and Mo. As a result, the alloying elements distribute evenly in the ASB. In contrast, the dramatic adiabatic shear of bimodal alloy might give rise to the complete lamination of the globular primary α grain and the equiaxial prior β grain, which is accompanied by the dynamic recrystallization of α lamellae and β lamellae. As a result, ASB of bimodal alloy is composed of α/β nano-multilayers. Chemical redistribution does not occur in ASB of bimodal alloy. Bimodal Ti-5553 alloy should be a promising candidate for high performance armors with high mass efficiency due to the processes high dynamic flow stress and excellent ASB-resistance.